# N922TW: 1981 Mcdonnell Douglas DC-9-82(MD-82), registration cancelled 2017-09-19 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: September 19, 2017 - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas DC-9-82(MD-82)](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82) (registry code 3022082) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs) - Serial number: 48013 - Year built: 1981 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: June 20, 1997 - Certificate issued: November 23, 2015 - Last registry action: November 23, 2015 - Mode S code: ACC756 - Owner when cancelled: [Frontera Flight Holdings Inc](https://openairdocs.org/faa-owner/FRONTERA%20FLIGHT%20HOLDINGS%20INC) - Location: [Dover, DE](https://openairdocs.org/faa-place/DE/Dover) - Owner type: Corporation - Owner's area on the map: 39.1815° N, 75.4736° W: Placed by OpenAirDocs at the center of ZIP code 19901, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N922TW - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=922TW - Page: https://openairdocs.org/deregistered/N922TW-2017-09-19 From the FAA registry file of November 4, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe. ADs and bulletins for the Mcdonnell Douglas DC-9-82(MD-82): https://openairdocs.org/model/mcdonnell-douglas-dc-9-82-md-82.md ## Service difficulty reports (44) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR ZW0A0303202](https://openairdocs.org/sdr/ZW0A0303202), Mar 17, 2003: BATTERY PACK. INOPERATIVE. THE OVERHEAD EMERGENCY LIGHTS AT THE LEFT SIDE NUMBER 2 CABIN DOOR AND JUST BEHIND THE DOOR, AND THE LEFT AND RIGHT EMERGENCY LAMPS IN TAIL AREA, WERE INOPERATI - [SDR ZW0A0203701](https://openairdocs.org/sdr/ZW0A0203701), Mar 27, 2002: APU. SMOKE IN CABIN FROM AIR CONDITIONING. REMOVED AND REPLACED APU. LAST CHECK C PERFORMED 23AUG2001 MCI --CLOSED-- - [SDR ZW0A0107205](https://openairdocs.org/sdr/ZW0A0107205), Aug 17, 2001: CHANNEL. CRACKED. DURING CHECK-C MAINT FOUND L-2 HAT SECTION CRACKED AT STA 1418, LT SIDE. REPAIRED PER 53-02 FIG 18. PRIMED AND PAINTED PER SRM 51-10-03. INSTALLED FASTENERS PER - [SDR ZW0A0106301](https://openairdocs.org/sdr/ZW0A0106301), Aug 6, 2001: STRUCTURE. DAMAGED. DURING MAINTENANCE A DEEP GROOVE WAS FOUND IN THE CUT OUT FOR THE MID CARGO DOOR HANDLE DUE TO WEAR. REPLACED DOOR HANDLE CUTOUT PER SPM 6-70-01. - [SDR ZW0A0105506](https://openairdocs.org/sdr/ZW0A0105506), Jul 20, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT FOUND CRACK IN LONGERON 20L ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20L PER ARA 17776. - [SDR ZW0A0105505](https://openairdocs.org/sdr/ZW0A0105505), Jul 20, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT LONGERON 20R HAD TWO CRACKS, ABOVE FLAP BUS CABLE PULLEYS, STA 1003. REPAIRED LONGERON 20R PER ARA 17777. - [SDR ZW0A0105703](https://openairdocs.org/sdr/ZW0A0105703), Jul 19, 2001: FITTING. BROKEN. DURING CHECK-C MAINT FOUND BROKEN FITTING, P/N 5956034-552, AT STA 788 BETWEEN LONGERON 27R AND 28R. REPLACED BROKEN FITTING. TREATED AND PRIMED AND INSTALLED P - [SDR ZW0A0105409](https://openairdocs.org/sdr/ZW0A0105409), Jul 17, 2001: FLOORBEAM. CORRODED. DURING CHECK-C MAINT IN THE AFT CABIN FOUND TOP OF FLOORBEAM STA 1322 WAS CORRODED AT LBL 15 TO SIDEWALL. REMOVED CORROSION MECHANICALLY PER SPM 6-80-1. INSTALL - [SDR ZW0A0105408](https://openairdocs.org/sdr/ZW0A0105408), Jul 17, 2001: DOUBLER. CORRODED. DURING CHECK-C MAINT FOUND FINGER DOUBLER CORRODED ON OTBD SIDE OF LONGERON 26L, STA 788, MID CARGO COMPT. REPLACED FINGER DOUBLER PER SPM 6-80-01 AND FASTENERS - [SDR ZW0A0105407](https://openairdocs.org/sdr/ZW0A0105407), Jul 17, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR TRACK, LBL 44, STA 1136 TO 1174, AND 1174 TO 1231. CLEANED MINOR CORROSION STA 1200 TO 1231 PER SPM 6-80-01. - [SDR ZW0A0105406](https://openairdocs.org/sdr/ZW0A0105406), Jul 17, 2001: INTERCOSTAL. CRACKED. DURING CHECK-C MAINT THE INTERCOSTAL BETWEEN FLOOR SUPPORTS AT STA 782, ZERO BL WAS CRACKED AND BROKEN. INSTALLED DOUBLER ON INTERCOSTAL. USED 4-5, 5-6, AND 5-7 - [SDR ZW0A0105305](https://openairdocs.org/sdr/ZW0A0105305), Jul 13, 2001: LONGERON. CRACKED. DURING CHECK-C MAINT ON LT SIDE OF CABIN FOUND CRACKS AT STA 160, LONGERON 3L AND 4L. REPAIRED PER SRM 53-02 FIG 18. - [SDR ZW0A0105304](https://openairdocs.org/sdr/ZW0A0105304), Jul 13, 2001: WEB. DAMAGED. DURING CHECK-C MAINT FOUND HOLE IN MEMBRANE UNDER CABIN FLOOR, STA 1090 AND LBL 45. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2. - [SDR ZW0A0105303](https://openairdocs.org/sdr/ZW0A0105303), Jul 13, 2001: FLOORBEAM. CRACKED. DURING CHECK-C MAINT FOUND CABIN FLOORBEAM FITTING CRACKED AT STA 1308, LBL 35. REMOVED AND REPLACED FITTING PER SRM 51-30-5. - [SDR ZW0A0105111](https://openairdocs.org/sdr/ZW0A0105111), Jul 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 170 TO 200, RBL 7. FOUND CORRODED BEYOND LIMITS AND FABRICATED NEW FLOOR SUPPORT. - [SDR ZW0A0105110](https://openairdocs.org/sdr/ZW0A0105110), Jul 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 194 TO 202, LBL 15. REMOVED OLD SUPPORT AND MADE NEW SUPPORT. - [SDR ZW0A0105109](https://openairdocs.org/sdr/ZW0A0105109), Jul 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 160 TO 200, LBL 7. REMOVED OLD FLOOR SUPPORT AND MADE NEW. - [SDR ZW0A0105108](https://openairdocs.org/sdr/ZW0A0105108), Jul 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 200, LBL 6 TO RBL 6. REMOVED OLD SUPPORT AND MADE NEW SUPPORT FROM STOCK. PAINTED AND ALODINED PER - [SDR ZW0A0105006](https://openairdocs.org/sdr/ZW0A0105006), Jul 12, 2001: FITTING. CRACKED. DURING CHECK-C MAINT IN THE NOSE GEAR WHEEL WELL FOUND CRACK IN FITTING AT STA 69, LBL 16, THE INBD FITTING AT PRESSURE PANEL. REMOVED CRACKED FITTING AND INSTA - [SDR ZW0A0105004](https://openairdocs.org/sdr/ZW0A0105004), Jul 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 185 TO 190, RBL 44. MADE AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2. - [SDR ZW0A0105003](https://openairdocs.org/sdr/ZW0A0105003), Jul 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 190 TO 194, RBL 44. MADE AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2. - [SDR ZW0A0105002](https://openairdocs.org/sdr/ZW0A0105002), Jul 12, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT AT STA 183, RBL 44. MADE AND INSTALLED NEW FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2. - [SDR ZW0A0105107](https://openairdocs.org/sdr/ZW0A0105107), Jul 11, 2001: SEAT TRACK. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON NUMBER 2 FLOOR TRACK AT RBL 22, STA 1080 TO 1250. REPLACED TRACK PER SPM 6-70-01 AND SRM 53-05, FIG 4. PRIMED PER SRM 51 - [SDR ZW0A0105106](https://openairdocs.org/sdr/ZW0A0105106), Jul 11, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT IN CABIN AT STA 180, RBL 8 TO 44. INSTALLED NEW SUPPORT PER SPM 6-70-01. INSTALLED FASTENERS PER SRM 51-30 - [SDR ZW0A0105105](https://openairdocs.org/sdr/ZW0A0105105), Jul 11, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION AT STA 198 AND RBL 44, AND AT STA 200 RBL 11. INSTALLED FLOOR SUPPORT AT BOTH LOCATIONS PER SPM 6-70-01 AND RIVETS PER SRM - [SDR ZW0A0105104](https://openairdocs.org/sdr/ZW0A0105104), Jul 11, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION IN CABIN AT RBL 11, STA 209. REMOVED SUPPORT AND MADE NEW PART PER DRAWING PL9936535 ITEM 57, AND INSTALLED WITH HI-LOKS PE - [SDR ZW0A0105005](https://openairdocs.org/sdr/ZW0A0105005), Jul 11, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION AT RBL 15, STA 200. MADE AND INSTALLED FLOOR SUPPORT PER SPM 6-70-01 AND SRM 51-30-2. - [SDR ZW0A0105103](https://openairdocs.org/sdr/ZW0A0105103), Jul 10, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON CABIN FLOOR SUPPORT, STA 1250, BETWEEN NUMBER 1 AND 2 CHAIR TRACKS, LBL 22 TO 44. FABRICATED AND INSTALLED NEW FLOOR SUP - [SDR ZW0A0104904](https://openairdocs.org/sdr/ZW0A0104904), Jul 8, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT FOUND CORROSION ON FLOOR SUPPORT FITTINGS AT RBL 55, STA 202, 217, AND 208. REMOVED AND REPLACED FITTINGS PER SPM 6-70-01 AND SRM 51-30-05. - [SDR ZW0A0104903](https://openairdocs.org/sdr/ZW0A0104903), Jul 8, 2001: FLOOR SUPPORT. CORRODED. DURING CHECK-C MAINT THE CABIN FLOOR SUPPORT AT STA 160 TO 200, LBL 55, WAS CORRODED. REMOVED CORRODED PART AND FABRICATED NEW SUPPORT AND INSTALLED PER SPM 6-7 - [SDR ZW0A0104902](https://openairdocs.org/sdr/ZW0A0104902), Jul 8, 2001: WEB. PUNCTURED. DURING CHECK-C MAINT FOUND PUNCTURE IN FLOOR MEMBRANE AT STA 196, LBL 55. INSTALLED DOUBLER REPAIR PER SRM 53-01, FIG 2. - [SDR ZW0A0104704](https://openairdocs.org/sdr/ZW0A0104704), Jul 2, 2001: ANGLE. CRACKED. DURING CHECK-C MAINT FOUND CRACK IN LT MAIN GEAR WHEEL WELL FWD SHELF ATTACH ANGLE, FWD LOWER INBD CORNER OF WHEEL WELL. REMOVED AND REPLACED ANGLE WITH FABRICA - [SDR TWAA0106302](https://openairdocs.org/sdr/TWAA0106302), Apr 8, 2001: WIRE. WORN. THE EGRESS LIGHTS WERE INOPERATIVE FROM CABIN ROW 15 TO 21. REPLACED POWER FLEX CABLE. CHECK-C 6-10-00 JFK. - [SDR TWAA0103801](https://openairdocs.org/sdr/TWAA0103801), Feb 27, 2001: CONNECTOR. DIRTY. THE EGRESS LIGHTS FROM CABIN ROWS 29 THRU 33, AND THE EMERGENCY LIGHTS IN THE TAIL COMPARTMENT, WERE INOPERATIVE. FOUND RIBBON LIGHTS WITH MOISTURE AND DIRT AT - [SDR TWAA0101913](https://openairdocs.org/sdr/TWAA0101913), Jan 23, 2001: BULKHEAD. BIRD STRIKE. ON TAKEOFF SUFFERED BIRD STRIKE AT THE RADOME AREA. THE RADOME BULKHEAD WEB AT STA 37 WAS DAMAGED. INSTALLED NEW BULKHEAD WEB WITH RIVETS AND HI-LOK''S PER SRM - [SDR TWAA9912102](https://openairdocs.org/sdr/TWAA9912102), Sep 3, 1999: POWER STRIP. INOP. DURING PRE-FLIGHT, FOUND EGRESS LIGHTS INOP AT ROW 7-15 AND 28 AFT. REPLACED POWER LIGHT STRIP. AC-12 STL 7-17-99. - [SDR TWAA9911002](https://openairdocs.org/sdr/TWAA9911002), Aug 8, 1999: POWER SUPPLY. INOP. THE EGRESS LIGHTS WERE ON ALL THE TIME FROM CABIN ROWS 15 TO 31. REPLACED THE POWER SUPPLY. CHECK-C 7-17-99 STL. - [SDR TWAA9910802](https://openairdocs.org/sdr/TWAA9910802), Jul 30, 1999: POWER SUPPLY. INOP. THE EGRESS LIGHTS ILLUMINATED IN FLIGHT WITH THE SWITCH IN THE ARM POSITION, FROM ROW 29 TO THE BACK OF THE CABIN. REPLACED THE POWER SUPPLY. CHECK-C 7-17-99 ST - [SDR TWAA9901505](https://openairdocs.org/sdr/TWAA9901505), Jan 24, 1999: LAMP. FAILED. FOUND THE EVACUATION CHUTE LIGHT INOPERATIVE AT THE FORWARD LT AND RT CABIN DOORS. REPLACED LAMP IN EACH. CHECK-C 7-18-98 STL. - [SDR TWAA9818904](https://openairdocs.org/sdr/TWAA9818904), Nov 23, 1998: BATTERY PACK. DISCHARGED. DURING PREFLIGHT, FOUND EGRESS LIGHTING INOP BETWEEN ROWS 2 TO 15. REPLACED NR 2 EGRESS BATTERY PACK. - [SDR TWAA9812301](https://openairdocs.org/sdr/TWAA9812301), Jul 27, 1998: TAIL CONE. DEFORMED. DURING C-CHECK, THE TAIL CONE FAILED TO RELEASE DURING ROUTINE CHECK. FOUND THE UPPER SECTION OF THE TAIL CONE WAS DISTORTED SO THAT THE FOUR ATTACH POINTS DID - [SDR TWAA9812127](https://openairdocs.org/sdr/TWAA9812127), Jul 18, 1998: ATTACT TEE. DAMAGED. DURING CHECK-C MAINT, FOUND APU RT SIDEWALL ATTACH T WITH END FLANGE CUT OFF WITH 3 ATTACH HOLES TO GAIN ACCESS. INSTALLED FILLERS AND DOUBLERS PER ARA 15416 AN - [SDR TWAA9812104](https://openairdocs.org/sdr/TWAA9812104), Jul 14, 1998: BULKHEAD FITTING. DAMAGED. DURING CHECK-C MAINT, FOUND THE AFT BULKHEAD T-FITTING DAMAGED. CRACK WAS 2.5 BY 1.7 AT AREA OF AFT JACK POINT. REMOVED AND REPLACED T AS PER SRM 53-03, FIG 37A - [SDR TWAA9712403](https://openairdocs.org/sdr/TWAA9712403), Oct 10, 1997: SOCKET. FAILED. JFK - FLT 780 - CABIN ATTENDANT REPORTED SMELL OF BURNING WIRE AT OVERWING AREA. OVERHEAD AND SIDE LIGHTS TURNED OFF AND SMELL DISSIPATED. LIGHT SOCKET WAS DEAC ## FAA accident and incident reports (1) From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model. - [Incident 20010123002429I](https://openairdocs.org/incident/20010123002429I), Jan 23, 2001: Doug DC982 (N922TW), St Louis, MO, Substantial damage. (-23)No narrative ## Other aircraft with N922TW - [Registered now](https://openairdocs.org/aircraft/N922TW): Cirrus Design SR22, S/N 11621, built 2026 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.